FR2852689B1 - METHOD AND INDICATOR FOR DISPLAYING ILLUSTRATING MARGIN INFORMATION ON AN AIRCRAFT - Google Patents

METHOD AND INDICATOR FOR DISPLAYING ILLUSTRATING MARGIN INFORMATION ON AN AIRCRAFT

Info

Publication number
FR2852689B1
FR2852689B1 FR0303413A FR0303413A FR2852689B1 FR 2852689 B1 FR2852689 B1 FR 2852689B1 FR 0303413 A FR0303413 A FR 0303413A FR 0303413 A FR0303413 A FR 0303413A FR 2852689 B1 FR2852689 B1 FR 2852689B1
Authority
FR
France
Prior art keywords
aircraft
indicator
displaying
margin information
current
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR0303413A
Other languages
French (fr)
Other versions
FR2852689A1 (en
Inventor
Pascal Vialleton
Martin Delporte
Jean Christophe Reinmuth
Jacques Rosay
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0303413A priority Critical patent/FR2852689B1/en
Priority to DE602004001077T priority patent/DE602004001077T2/en
Priority to AT04290545T priority patent/ATE329231T1/en
Priority to EP04290545A priority patent/EP1460385B1/en
Priority to CA2460608A priority patent/CA2460608C/en
Priority to US10/800,916 priority patent/US6982655B2/en
Publication of FR2852689A1 publication Critical patent/FR2852689A1/en
Application granted granted Critical
Publication of FR2852689B1 publication Critical patent/FR2852689B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00Arrangements or adaptations of instruments
    • B64D43/02Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • G01C23/005Flight directors
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D7/00Indicating measured values

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Traffic Control Systems (AREA)
  • Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

The method involves determining a current incidence of an aircraft, and defining a longitudinal scale (10) that depends on a current aerodynamic configuration of the aircraft. The longitudinal scale is presented on a visual display unit, where the scale is longitudinally moved with respect to the current incidence of the aircraft that is illustrated by a characteristic sign (15) fixed on the display unit. An independent claim is also included for an indication device for indicating a speed of an aircraft.
FR0303413A 2003-03-20 2003-03-20 METHOD AND INDICATOR FOR DISPLAYING ILLUSTRATING MARGIN INFORMATION ON AN AIRCRAFT Expired - Fee Related FR2852689B1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR0303413A FR2852689B1 (en) 2003-03-20 2003-03-20 METHOD AND INDICATOR FOR DISPLAYING ILLUSTRATING MARGIN INFORMATION ON AN AIRCRAFT
DE602004001077T DE602004001077T2 (en) 2003-03-20 2004-03-01 Method and device for displaying speed ranges in an aircraft
AT04290545T ATE329231T1 (en) 2003-03-20 2004-03-01 METHOD AND DEVICE FOR DISPLAYING SPEED RANGES IN AN AIRCRAFT
EP04290545A EP1460385B1 (en) 2003-03-20 2004-03-01 Method of and device for displaying information representing speed ranges on an aircraft
CA2460608A CA2460608C (en) 2003-03-20 2004-03-09 Procedure and indicator for displaying information indicating speed margins for an aircraft
US10/800,916 US6982655B2 (en) 2003-03-20 2004-03-16 Method and indicator for displaying information showing the airspeed tolerance margins for an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0303413A FR2852689B1 (en) 2003-03-20 2003-03-20 METHOD AND INDICATOR FOR DISPLAYING ILLUSTRATING MARGIN INFORMATION ON AN AIRCRAFT

Publications (2)

Publication Number Publication Date
FR2852689A1 FR2852689A1 (en) 2004-09-24
FR2852689B1 true FR2852689B1 (en) 2005-06-10

Family

ID=32799699

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0303413A Expired - Fee Related FR2852689B1 (en) 2003-03-20 2003-03-20 METHOD AND INDICATOR FOR DISPLAYING ILLUSTRATING MARGIN INFORMATION ON AN AIRCRAFT

Country Status (6)

Country Link
US (1) US6982655B2 (en)
EP (1) EP1460385B1 (en)
AT (1) ATE329231T1 (en)
CA (1) CA2460608C (en)
DE (1) DE602004001077T2 (en)
FR (1) FR2852689B1 (en)

Families Citing this family (21)

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US7689324B1 (en) * 2004-06-21 2010-03-30 Rockwell Collins, Inc. Aircraft capability and hazard zone interface and method
US8027758B2 (en) 2005-01-19 2011-09-27 Airbus Operations (S.A.S.) Navigation system for an aircraft and associated command process
FR2930053B1 (en) 2008-04-14 2013-09-20 Airbus France METHOD AND DEVICE FOR GUIDING AN AIRCRAFT
US8451144B2 (en) * 2009-02-04 2013-05-28 Honeywell International Inc. Flaps overspeed advisory system
US8600586B2 (en) * 2009-02-04 2013-12-03 Honeywell International Inc. Stable approach monitor (SAM) system
BR112012017154B1 (en) * 2009-12-21 2021-09-28 The Boeing Company METHOD OF CONTROLLING THE TILT ATTITUDE OF A MULTIMOTOR AIRCRAFT EXPERIMENTING PUSH AND SYSTEM ASYMMETRY FOR A MULTIMOTOR AIRCRAFT
US8630752B2 (en) * 2011-09-08 2014-01-14 Honeywell International Inc. System and method of displaying airspeed information for an aircraft
CN103206960B (en) * 2012-01-13 2016-04-27 北京四维图新科技股份有限公司 A kind of method for path navigation and device
US8653990B2 (en) * 2012-06-18 2014-02-18 The Boeing Company Stall management system
FR2996635B1 (en) * 2012-10-08 2015-08-07 Airbus Operations Sas METHOD AND DEVICE FOR DISPLAYING FLIGHT PARAMETERS ON AN AIRCRAFT.
WO2014062984A1 (en) 2012-10-17 2014-04-24 Dugan Brian M Methods and apparatus for reducing anxiety during travel
US20140121863A1 (en) * 2012-10-29 2014-05-01 The Boeing Company Flight Envelope Display
US9193473B2 (en) * 2013-09-20 2015-11-24 Safe Flight Instrument Corporation Angle of attack display
US10227140B2 (en) 2014-07-11 2019-03-12 Cmc Electronics Inc System and method for detecting and alerting the user of an aircraft of an impendent adverse condition
CN107980031B (en) * 2015-04-07 2021-08-24 阿斯潘航空电子有限公司 System and method for angle of attack indication without dedicated sensors and aircraft information
FR3036835B1 (en) 2015-06-01 2017-06-23 Airbus Operations Sas METHOD AND DEVICE FOR ENABLING THE DISPLAY OF AT LEAST ONE MARGIN INDICATOR TO REMOVE AN AIRCRAFT.
FR3054686B1 (en) * 2016-07-28 2018-08-03 Thales METHOD OF GRAPHIC MANAGEMENT OF SYMBOLOGY IN A THREE DIMENSIONAL SYNTHETIC VIEW OF THE OUTSIDE LANDSCAPE IN AN AIRCRAFT VISUALIZATION SYSTEM
US11010941B1 (en) 2018-12-19 2021-05-18 EffectiveTalent Office LLC Matched array general talent architecture system and method
US10803085B1 (en) * 2018-12-19 2020-10-13 Airspeed Systems LLC Matched array airspeed and angle of attack alignment system and method
US10896529B1 (en) 2018-12-19 2021-01-19 EffectiveTalent Office LLC Matched array talent architecture system and method
US11016988B1 (en) 2018-12-19 2021-05-25 Airspeed Systems LLC Matched array flight alignment system and method

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4149148A (en) * 1977-04-19 1979-04-10 Sperry Rand Corporation Aircraft flight instrument display system
US4638437A (en) * 1984-06-25 1987-01-20 The Boeing Company Aircraft performance margin indicator
FR2730841B1 (en) * 1995-02-17 1997-04-25 Sextant Avionique AIRCRAFT MONITORING AND GUIDANCE METHOD AND DEVICE FOR PRECISION LANDING
US6131055A (en) * 1998-12-11 2000-10-10 The Boeing Company Aircraft non-normalized angle-of-attack indicating system
WO2000065423A2 (en) * 1999-04-01 2000-11-02 Price Ricardo A Electronic flight instrument displays
US6262674B1 (en) * 2000-08-10 2001-07-17 Honeywell International Inc. Aircraft display with potential thrust indicator

Also Published As

Publication number Publication date
US6982655B2 (en) 2006-01-03
DE602004001077D1 (en) 2006-07-20
ATE329231T1 (en) 2006-06-15
CA2460608C (en) 2012-05-22
FR2852689A1 (en) 2004-09-24
CA2460608A1 (en) 2004-09-20
EP1460385A1 (en) 2004-09-22
US20040183699A1 (en) 2004-09-23
DE602004001077T2 (en) 2006-11-30
EP1460385B1 (en) 2006-06-07

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Legal Events

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ST Notification of lapse

Effective date: 20111130